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Description
| - A module for an aerometric values computation consists of a differential pressure sensor Freescale MPXV7002DP (DPS), an absolute pressure sensor Freescale MPXA4115A (APS), a temperature sensor Analog Devices TMP36, a control board (CB) with a microprocessor Freescale MC9S12XDT and of a Pitot-static probe (PSP). PSP is connected with pressure sensors by silicon tubes, so that the APS measures a static pressure and the DPS measures a dynamic pressure. CB processes sensors output voltage with its inner AD converters and provides data filtering by a digital filter and the computation of determinate aerometric values. These values are: the static pressure, the dynamic pressure, a temperature of an ambient air, an indicated air speed, an altitude and a vertical speed. These measured and computed values are sent through a CAN bus in a CANaerospace format to a superior system, which can be represented by a central control module or by PC including a Matlab program providing required interface. The functional prototype is the result of the project MSM6840770015, partial task %22Microsensors in aeronautics%22.
- A module for an aerometric values computation consists of a differential pressure sensor Freescale MPXV7002DP (DPS), an absolute pressure sensor Freescale MPXA4115A (APS), a temperature sensor Analog Devices TMP36, a control board (CB) with a microprocessor Freescale MC9S12XDT and of a Pitot-static probe (PSP). PSP is connected with pressure sensors by silicon tubes, so that the APS measures a static pressure and the DPS measures a dynamic pressure. CB processes sensors output voltage with its inner AD converters and provides data filtering by a digital filter and the computation of determinate aerometric values. These values are: the static pressure, the dynamic pressure, a temperature of an ambient air, an indicated air speed, an altitude and a vertical speed. These measured and computed values are sent through a CAN bus in a CANaerospace format to a superior system, which can be represented by a central control module or by PC including a Matlab program providing required interface. The functional prototype is the result of the project MSM6840770015, partial task %22Microsensors in aeronautics%22. (en)
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Title
| - Module for Aerometric Values Computing on UAV
- Module for Aerometric Values Computing on UAV (en)
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skos:prefLabel
| - Module for Aerometric Values Computing on UAV
- Module for Aerometric Values Computing on UAV (en)
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skos:notation
| - RIV/68407700:21220/11:00187309!RIV12-MSM-21220___
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
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http://linked.open...vai/riv/dodaniDat
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http://linked.open...aciTvurceVysledku
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http://linked.open.../riv/druhVysledku
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http://linked.open...iv/duvernostUdaju
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http://linked.open...onomickeParametry
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http://linked.open...titaPredkladatele
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http://linked.open...dnocenehoVysledku
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http://linked.open...ai/riv/idVysledku
| - RIV/68407700:21220/11:00187309
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http://linked.open...terniIdentifikace
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http://linked.open...riv/jazykVysledku
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http://linked.open...vai/riv/kategorie
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http://linked.open.../riv/klicovaSlova
| - Air Data Computer; CANaerospace (en)
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http://linked.open.../riv/klicoveSlovo
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http://linked.open...ontrolniKodProRIV
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http://linked.open.../licencniPoplatek
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http://linked.open...okalizaceVysledku
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http://linked.open...in/vavai/riv/obor
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http://linked.open...ichTvurcuVysledku
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http://linked.open...cetTvurcuVysledku
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http://linked.open...UplatneniVysledku
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http://linked.open...echnickeParametry
| - Zařízení měří statický tlak (rozsah 100 kPa), dynamický tlak (rozsah 4kPa), teplotu (rozsah 165 C), výšku letu (rozsah 14 km), indikovanou rychlost (rozsah +-200 km/h) a vertikální rychlost (rozsah +- 50 m/s).
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http://linked.open...iv/tvurceVysledku
| - Roháč, Jan
- Pačes, Pavel
- Popelka, Jan
- Čenský, Tomáš
- Papaj, Jan
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http://linked.open...avai/riv/vlastnik
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http://linked.open...itiJinymSubjektem
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http://linked.open...n/vavai/riv/zamer
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http://localhost/t...ganizacniJednotka
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